CN103532274A - Hydraulic turbine generator rotor spider with flange hub - Google Patents
Hydraulic turbine generator rotor spider with flange hub Download PDFInfo
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- CN103532274A CN103532274A CN201310509589.3A CN201310509589A CN103532274A CN 103532274 A CN103532274 A CN 103532274A CN 201310509589 A CN201310509589 A CN 201310509589A CN 103532274 A CN103532274 A CN 103532274A
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Abstract
The invention discloses a hydraulic turbine generator rotor spider with a flange hub, which comprises a rotor hub, a yoke ring, a plurality of oblique support arms supported between the rotor hub and the yoke ring, and oblique rib plates welded between the adjacent oblique support arms, wherein an area between an excircle of the rotor hub and the yoke ring is divided into a plurality of ventilation ducts by the oblique support arms; the ventilation ducts are internally provided with flange rib plates for flow equalization and guide of air flows before and behind the rotor hub; and the flange rib plates are supported between the adjacent oblique support arms and the rotor hub. The rotor spider has the advantages that the rotor spider is simple in structure and high in strength and can ensure ventilation quantity.
Description
Technical field
The present invention relates generally to hydraulic generator, relates in particular to a kind of rotor support power generator with edge of a wing wheel hub.
Background technology
Bulb Turbine Units generator rotor support is generally comprised of wheel hub disk, support arm and cylindrical shape yoke ring.Rotor field spider is flexible tiltedly support arm structure, it is a vitals of generator rotating part, it is connected with macro-axis with magnetic pole respectively, and when generator normally moves, rotor field spider will bear moment of torsion, the gravity of self and the effect of centrifugal force, is the parts of a stressed complexity.
Known Buddhist nun that, Guigang, the generator rotor support of Chai Jiaxia and Hongjiang power plant is all to adopt table roller (wheel hub), oblique support arm structure, for Alstom, (former Switzerland ABB AB produces the factory of hydraulic generator, the purchase of Hou Bei Alstom) traditional structure, once be widely used in the vertical unit of water power (as Three Gorges etc.) and bulb-type unit, all there is rotor field spider support arm breakage problem in above-mentioned several power plant (being bulb-type unit), Ling Jin beach rotor field spider is the table roller (wheel hub) of Hitachi, Ltd's design, allotment arm configuration, also there is support arm breakage problem, as 6 46MW scaled bulb tubular hydraulic generators of Hongjiang Installation in Plant, #1～#6 unit is gone into operation for 2003, #6 unit is gone into operation for 2006.Since 2009, there is successively gusset buckling phenomenon in 6 set generator rotor field spiders, also there is the situation of rotor field spider support arm gusset fracture in #4, #6 unit, serious threat is to the safe operation of main equipment, and first large-scale bulb formula unit Jiangkou rotor field spider breathing out electricity manufacture adopts double-disc structure, within 1998, put into operation, rotor field spider seminess does not occur so far.The follow-up safflower putting into operation, Kang Yang, Changzhou, India bamboo draw the units such as orchid, bright spirit, large holder mountain also not find crack problem.The rotor field spider rigidity of proof double-disc structure is better than table roller structure, greatly reduces the destruction of alternate load to rotor field spider.For guaranteeing that rotary piston machine shelf structure has enough Rigidity and strengths, is necessary it to carry out strength Calculation Improvement scheme, analytical calculation improvement effect.
Summary of the invention
The technical problem to be solved in the present invention is to overcome the deficiencies in the prior art, provide a kind of simple in structure, intensity is high, can guarantee the rotor support power generator with edge of a wing wheel hub of ventilation quantity.
For solving the problems of the technologies described above, the present invention by the following technical solutions:
A kind of rotor support power generator with edge of a wing wheel hub, comprise rotor hub, yoke ring, be supported in a plurality of bearing diagonal arms between rotor hub and yoke ring and be welded in the diagonal bar plate between adjacent bearing diagonal arm, between described rotor hub cylindrical and yoke ring, by bearing diagonal arm, be separated into a plurality of ventilating hole channels, in each ventilating hole channel, be provided with the air-flow before and after rotor hub is carried out to current-sharing guiding edge of a wing gusset, described edge of a wing gusset is supported between adjacent bearing diagonal arm and rotor hub.
Further improvement as technique scheme:
Described edge of a wing gusset comprises long end portion, short end portion, curved portions and the diversion division from long end portion to short end portion smooth transition, described curved portions is connected with rotor hub cylindrical, the ventilation unit of described diversion division and ventilating hole channel is adjacent, described long end portion is connected respectively a bearing diagonal arm with short end portion, and the direction of rotation along described rotor support power generator, short end portion is positioned at the place ahead, and long end portion is positioned at rear.
Described diagonal bar plate one end is connected with the centre position of bearing diagonal arm, and the long end portion of described edge of a wing gusset and the link position of bearing diagonal arm extend beyond the centre position of described bearing diagonal arm.The long end portion of described edge of a wing gusset is connected with the short end portion of another edge of a wing gusset in adjacent ventilating hole channel.
Described long end portion is provided with the first male portion and the first recess, described short end portion is provided with the second male portion and the second recess, described edge of a wing gusset docks and is welded to connect with the second male portion of another edge of a wing gusset in adjacent ventilating hole channel in the first male portion, and described edge of a wing gusset is welded to connect with adjacent bearing diagonal arm respectively in the first recess and the second recess edge.
Described diversion division comprises that described convex arc section is connected with concave arc-shaped section smooth transition near the convex arc section of short end portion with near the concave arc-shaped section of long end portion.
Between described adjacent bearing diagonal arm, be provided with two diagonal bar plates, described two diagonal bar plates are divided into gusset both sides, the described edge of a wing, and each diagonal bar plate and described edge of a wing gusset are welded to connect.
Described edge of a wing gusset is steel edge of a wing gusset.
Compared with prior art, the invention has the advantages that:
The rotor support power generator with edge of a wing wheel hub of the present invention, between rotor hub cylindrical and yoke ring, by bearing diagonal arm, be separated into a plurality of ventilating hole channels, and in each ventilating hole channel, be provided with edge of a wing gusset, edge of a wing gusset is supported between adjacent bearing diagonal arm and rotor hub, it is simple in structure, be easy to realize, compared with only supporting by diagonal bar plate between traditional adjacent bearing diagonal arm, this edge of a wing gusset belongs to the extension of rotor hub, contact area and the bearing length to bearing diagonal arm of rotor hub and bearing diagonal arm have been expanded, greatly improved the support strength of bearing diagonal arm and rigidity, suppress when unit is unloaded and overrun without the centrifugal force in electromagnetic braking moment situation, and the bearing diagonal brachiocylloosis metaboly that causes of the torsional interaction that hydraulic turbine blades resistance and generator moment of inertia produce mutually while shutting down, extended useful life.And this edge of a wing gusset can carry out current-sharing guiding to the air-flow before and after rotor hub, guaranteed wind speed and the ventilation quantity in ventilating hole channel, limited to greatest extent the ventilating hole channel area that brings due to edge of a wing gusset reduce airflow value is reduced, therefore in general structure strength increase situation, farthest reduced the impact of edge of a wing wheel hub on the cooling effect of each heat generating components of generator.
Accompanying drawing explanation
Fig. 1 is the structural representation that the present invention has the rotor support power generator of edge of a wing wheel hub.
Fig. 2 is the structural representation that the present invention has edge of a wing gusset in the rotor support power generator of edge of a wing wheel hub.
Fig. 3 is that the present invention has the structural representation after two edge of a wing link of boards in the rotor support power generator of edge of a wing wheel hub.
Fig. 4 is the structural representation after the present invention has edge of a wing gusset in the rotor support power generator of edge of a wing wheel hub and is connected with rotor hub.
Fig. 5 is the structural representation that the present invention has bearing diagonal arm in the rotor support power generator of edge of a wing wheel hub.
Fig. 6 is the structural representation that the present invention has diagonal bar plate in the rotor support power generator of edge of a wing wheel hub.
In figure, each label represents:
1, rotor hub; 2, yoke ring; 3, bearing diagonal arm; 4, diagonal bar plate; 5, ventilating hole channel; 6, edge of a wing gusset; 61, long end portion; 611, the first male portion; 612, the first recess; 62, short end portion; 621, the second male portion; 622, the second recess; 63, curved portions; 64, diversion division; 641, convex arc section; 642, concave arc-shaped section.
Embodiment
Below with reference to Figure of description and specific embodiment, the present invention is described in further details.
Fig. 1 to Fig. 6 shows the rotor support power generator embodiment with edge of a wing wheel hub of the present invention, this rotor field spider comprises rotor hub 1, yoke ring 2, be supported in a plurality of bearing diagonal arms 3 between rotor hub 1 and yoke ring 2 and be welded in the diagonal bar plate 4 between adjacent bearing diagonal arm 3, between rotor hub 1 cylindrical and yoke ring 2, by bearing diagonal arm 3, be separated into a plurality of ventilating hole channels 5, in each ventilating hole channel 5, be provided with edge of a wing gusset 6, edge of a wing gusset 6 is supported between adjacent bearing diagonal arm 3 and rotor hub 1, it is simple in structure, be easy to realize, compared with only supporting by diagonal bar plate 4 between traditional adjacent bearing diagonal arm 3, this edge of a wing gusset 6 belongs to the extension of rotor hub 1, expanded contact area and the bearing length to bearing diagonal arm 3 of rotor hub 1 with bearing diagonal arm 3, greatly improved the support strength of bearing diagonal arm 3 and rigidity, suppress when unit is unloaded and overrun without the centrifugal force in electromagnetic braking moment situation, and the bearing diagonal arm 3 flexural deformation phenomenons that cause of the torsional interaction that hydraulic turbine blades resistance and generator moment of inertia produce mutually while shutting down, extended useful life.And this edge of a wing gusset 6 can be to carrying out current-sharing guiding to the air-flow of rotor hub 1 front and back, wind speed and ventilation quantity in ventilating hole channel 5 have been guaranteed, limited to greatest extent ventilating hole channel 5 volumes that bring due to edge of a wing gusset 6 reduce airflow value is reduced, therefore in general structure strength increase situation, this edge of a wing gusset 6 has farthest reduced the impact of edge of a wing wheel hub on the cooling effect of each heat generating components of generator.
In the present embodiment, edge of a wing gusset 6 further comprises long end portion 61, short end portion 62, curved portions 63 and the diversion division 64 from long end portion 61 to short end portion 62 smooth transition, curved portions 63 is welded to connect with rotor hub 1 cylindrical, diversion division 64 is adjacent with the ventilation unit of ventilating hole channel 5, long end portion 61 and short end portion 62 are welded to connect respectively a bearing diagonal arm 3, and the direction of rotation along rotor support power generator, short end portion 62 is positioned at the place ahead, long end portion 61 is positioned at rear, when rotor support power generator rotates (as shown in Figure 1, the direction of arrow is direction of rotation), air-flow flows into from being positioned at the short end portion 62 in the place ahead, and flow to long end portion 61 and discharge from the upper side along diversion division 64, air-flow in 64 pairs of ventilating hole channels 5 of this diversion division plays good guide effect, wind speed and ventilation quantity in ventilating hole channel 5 have been guaranteed, limited to greatest extent reducing of airflow value, by the calculating to apparatus for electrical generator ventilation system, original structure airflow value is 27.07m
3/ s is 26.37m and adopt this airflow value with the rotor field spider of the edge of a wing gusset 6 of diversion division 64
3/ s, total blast volume changes little, and therefore, in general structure strength increase situation, this diversion division 64 has farthest reduced the impact of edge of a wing gusset 6 on the cooling effect of each heat generating components of generator.
In the present embodiment, diagonal bar plate 4 one end are connected with the centre position of bearing diagonal arm 3, the long end portion 61 of edge of a wing gusset 6 and the link position of bearing diagonal arm 3 extend beyond the centre position of bearing diagonal arm 3, diagonal bar plate 4 at one end can be welded to connect with the centre position of bearing diagonal arm 3, when bearing diagonal arm 3 is played a supporting role, make bearing diagonal arm 3 stress concentrate on centre position, this position is comparatively weak, easy bending, and long end portion 61 is just supported in bearing diagonal arm 3 in comparatively weak centre position, finely shared the stress that 4 pairs of bearing diagonal arms 3 of diagonal bar plate produce, improved intensity.
In the present embodiment, in the long end portion 61 of edge of a wing gusset 6 and adjacent ventilating hole channel 5, the short end portion 62 of another edge of a wing gusset 6 is welded to connect, be that edge of a wing gusset 6 is welded to connect along rotor hub 1 cylindrical, and adjacent edge of a wing gusset 6 is welded to connect equally, make edge of a wing gusset 6 and rotor hub 1 form an overall structure, extended the diameter of this table roller construction rotor wheel hub 1, to strengthen the rigidity of rotor field spider, this rotor hub 1 with edge of a wing gusset 6 is optimized the integrated support intensity of rotor field spider.
In the present embodiment, long end portion 61 is provided with the first male portion 611 and the first recess 612, short end portion 62 is provided with the second male portion 621 and the second recess 622, edge of a wing gusset 6 docks and is welded to connect with the second male portion 621 of another edge of a wing gusset 6 in adjacent ventilating hole channel 5 in the first male portion 611, and edge of a wing gusset 6 is welded to connect with adjacent bearing diagonal arm 3 respectively in the first recess 612 and the second recess 622 edges.
In the present embodiment, in long end portion 61, be further provided with the first male portion 611 and the first recess 612, short end portion 62 is provided with the second male portion 621 and the second recess 622, edge of a wing gusset 6 docks and is welded to connect with the second male portion 621 of another edge of a wing gusset 6 in adjacent ventilating hole channel 5 in the first male portion 611, adjacent edge of a wing gusset 6 is linked together and be convenient to assembly welding on rotor hub 1, very convenient during welding, edge of a wing gusset 6 is welded to connect with two adjacent bearing diagonal arms 3 respectively in the first recess 612 and the second recess 622 edges, make again edge of a wing gusset 6 and bearing diagonal arm 3 link together, well shared the abutment pressure of bearing diagonal arm 3 and diagonal bar plate 4, improved whole support performance of rotor field spider.
In the present embodiment, diversion division 64 comprises near the convex arc section 641 of short end portion 62 with near the concave arc-shaped section 642 of long end portion 61, it is simple in structure, be convenient to moulding, convex arc section 641 is connected with concave arc-shaped section 642 smooth transition, air-flow is played to good guide effect, guaranteed wind speed and ventilation quantity in ventilating hole channel 5.
In the present embodiment, between adjacent bearing diagonal arm 3, be provided with 4, two diagonal bar plates 4 of two diagonal bar plates and be divided into edge of a wing gusset 6 both sides, each diagonal bar plate 4 is welded to connect with edge of a wing gusset 6, further alleviate the abutment pressure of diagonal bar plate 4, can effectively prevent even fracture of diagonal bar plate 4 distortion.
In the present embodiment, edge of a wing gusset 6 is steel edge of a wing gusset, and steel material has been guaranteed the Rigidity and strength of this edge of a wing gusset 6, has effectively promoted the weight capacity of rotor field spider.
Although the present invention discloses as above with preferred embodiment, yet not in order to limit the present invention.Any those of ordinary skill in the art, in the situation that not departing from technical solution of the present invention scope, can utilize the technology contents of above-mentioned announcement to make many possible changes and modification to technical solution of the present invention, or be revised as the equivalent embodiment of equivalent variations.Therefore, every content that does not depart from technical solution of the present invention,, all should drop in the scope of technical solution of the present invention protection any simple modification made for any of the above embodiments, equivalent variations and modification according to the technology of the present invention essence.
Claims (10)
1. a rotor support power generator with edge of a wing wheel hub, comprise rotor hub (1), yoke ring (2), be supported in a plurality of bearing diagonal arms (3) between rotor hub (1) and yoke ring (2) and be welded in the diagonal bar plate (4) between adjacent bearing diagonal arm (3), between described rotor hub (1) cylindrical and yoke ring (2), by bearing diagonal arm (3), be separated into a plurality of ventilating hole channels (5), it is characterized in that: in each ventilating hole channel (5), be provided with the edge of a wing gusset (6) that the air-flow before and after rotor hub (1) is carried out to current-sharing guiding, described edge of a wing gusset (6) is supported between adjacent bearing diagonal arm (3) and rotor hub (1).
2. the rotor support power generator with edge of a wing wheel hub according to claim 1, it is characterized in that: described edge of a wing gusset (6) comprises long end portion (61), short end portion (62), curved portions (63) and the diversion division (64) from long end portion (61) to short end portion (62) smooth transition, described curved portions (63) is connected with rotor hub (1) cylindrical, described diversion division (64) is adjacent with the ventilation unit of ventilating hole channel (5), described long end portion (61) is connected respectively a bearing diagonal arm (3) with short end portion (62), and the direction of rotation along described rotor support power generator, short end portion (62) is positioned at the place ahead, long end portion (61) is positioned at rear.
3. the rotor support power generator with edge of a wing wheel hub according to claim 2, it is characterized in that: described diagonal bar plate (4) one end is connected with the centre position of bearing diagonal arm (3), the long end portion (61) of described edge of a wing gusset (6) and the link position of bearing diagonal arm (3) extend beyond the centre position of described bearing diagonal arm (3).
4. the rotor support power generator with edge of a wing wheel hub according to claim 3, is characterized in that: the long end portion (61) of described edge of a wing gusset (6) is connected with the short end portion (62) of another edge of a wing gusset (6) in adjacent ventilating hole channel (5).
5. the rotor support power generator with edge of a wing wheel hub according to claim 4, it is characterized in that: described long end portion (61) is provided with the first male portion (611) and the first recess (612), described short end portion (62) is provided with the second male portion (621) and the second recess (622), described edge of a wing gusset (6) docks and is welded to connect with second male portion (621) of another edge of a wing gusset (6) in adjacent ventilating hole channel (5) in the first male portion (611), described edge of a wing gusset (6) is welded to connect with adjacent bearing diagonal arm (3) respectively in the first recess (612) and the second recess (622) edge.
6. according to the rotor support power generator with edge of a wing wheel hub described in any one in claim 2 to 5, it is characterized in that: described diversion division (64) comprises that described convex arc section (641) is connected with concave arc-shaped section (642) smooth transition near the concave arc-shaped section (642) of the convex arc section (641) of short end portion (62) and close long end portion (61).
7. according to the rotor support power generator with edge of a wing wheel hub described in claim 1 to 5 any one, it is characterized in that: between described adjacent bearing diagonal arm (3), be provided with two diagonal bar plates (4), described two diagonal bar plates (4) are divided into described edge of a wing gusset (6) both sides, and each diagonal bar plate (4) is welded to connect with described edge of a wing gusset (6).
8. the rotor support power generator with edge of a wing wheel hub according to claim 6, it is characterized in that: between described adjacent bearing diagonal arm (3), be provided with two diagonal bar plates (4), described two diagonal bar plates (4) are divided into described edge of a wing gusset (6) both sides, and each diagonal bar plate (4) is welded to connect with described edge of a wing gusset (6).
9. according to the rotor support power generator with edge of a wing wheel hub described in claim 1 to 5 any one, it is characterized in that: described edge of a wing gusset (6) is steel edge of a wing gusset.
10. the rotor support power generator with edge of a wing wheel hub according to claim 8, is characterized in that: described edge of a wing gusset (6) is steel edge of a wing gusset.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310509589.3A CN103532274B (en) | 2013-10-25 | 2013-10-25 | There is the rotor support power generator of edge of a wing wheel hub |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310509589.3A CN103532274B (en) | 2013-10-25 | 2013-10-25 | There is the rotor support power generator of edge of a wing wheel hub |
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| CN103532274A true CN103532274A (en) | 2014-01-22 |
| CN103532274B CN103532274B (en) | 2016-03-30 |
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| CN201310509589.3A Expired - Fee Related CN103532274B (en) | 2013-10-25 | 2013-10-25 | There is the rotor support power generator of edge of a wing wheel hub |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104113183A (en) * | 2014-07-28 | 2014-10-22 | 泰乐玛汽车制动***（上海）有限公司 | Efficient heat dissipation rotor and eddy current retarder with same |
| CN104333161A (en) * | 2014-11-27 | 2015-02-04 | 天津市天发重型水电设备制造有限公司 | Connecting method of hydro generator rotor support |
| CN103904802B (en) * | 2014-04-17 | 2016-06-08 | 张家港倍恩特磁塑科技有限公司 | Washing machine direct current generator outer rotor |
| CN105914928A (en) * | 2016-07-08 | 2016-08-31 | 东方电气集团东方电机有限公司 | Ventilation adjustable hydraulic generator rotor bracket |
| CN106052634A (en) * | 2016-08-05 | 2016-10-26 | 怀化沅江电力开发有限责任公司洪江水力发电厂 | Level gauge-based water turbine blade rotation angle measurement method |
| CN108599424A (en) * | 2018-06-13 | 2018-09-28 | 哈尔滨理工大学 | Pumped-storage power generation motor with multistage adding pressure type rotor step by step |
| CN112994337A (en) * | 2021-02-20 | 2021-06-18 | 浙江富春江水电设备有限公司 | Fluid machinery rotating part stress self-adaptation structure |
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| CN203617807U (en) * | 2013-10-25 | 2014-05-28 | 怀化沅江电力开发有限责任公司洪江水力发电厂 | Hydraulic turbine generator rotor spider with flange hub |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103904802B (en) * | 2014-04-17 | 2016-06-08 | 张家港倍恩特磁塑科技有限公司 | Washing machine direct current generator outer rotor |
| CN104113183B (en) * | 2014-07-28 | 2019-07-26 | 泰乐玛汽车制动***（上海）有限公司 | A kind of rotor of high efficiency and heat radiation and current vortex retarder using the rotor |
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| CN104333161A (en) * | 2014-11-27 | 2015-02-04 | 天津市天发重型水电设备制造有限公司 | Connecting method of hydro generator rotor support |
| CN105914928A (en) * | 2016-07-08 | 2016-08-31 | 东方电气集团东方电机有限公司 | Ventilation adjustable hydraulic generator rotor bracket |
| CN105914928B (en) * | 2016-07-08 | 2018-05-25 | 东方电气集团东方电机有限公司 | A kind of adjustable rotor support power generator of ventilation |
| CN106052634B (en) * | 2016-08-05 | 2018-08-10 | 怀化沅江电力开发有限责任公司洪江水力发电厂 | Hydraulic turbine blades Rotating Angle Measurement based on spirit level |
| CN106052634A (en) * | 2016-08-05 | 2016-10-26 | 怀化沅江电力开发有限责任公司洪江水力发电厂 | Level gauge-based water turbine blade rotation angle measurement method |
| CN108599424A (en) * | 2018-06-13 | 2018-09-28 | 哈尔滨理工大学 | Pumped-storage power generation motor with multistage adding pressure type rotor step by step |
| CN108599424B (en) * | 2018-06-13 | 2019-06-14 | 哈尔滨理工大学 | Pumped-storage power generation motor with multistage adding pressure type rotor step by step |
| CN112994337A (en) * | 2021-02-20 | 2021-06-18 | 浙江富春江水电设备有限公司 | Fluid machinery rotating part stress self-adaptation structure |
| CN114530979A (en) * | 2021-02-20 | 2022-05-24 | 浙江富春江水电设备有限公司 | Fluid machinery rotating part stress self-adaptation structure |
| CN114530979B (en) * | 2021-02-20 | 2023-12-12 | 浙江富春江水电设备有限公司 | Stress self-adaptive structure of fluid machinery rotating part |
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| CN103532274B (en) | 2016-03-30 |
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